EP1074636B1 - Use of aluminum alloy sheet for heat shielding - Google Patents

Use of aluminum alloy sheet for heat shielding Download PDF

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Publication number
EP1074636B1
EP1074636B1 EP00116579A EP00116579A EP1074636B1 EP 1074636 B1 EP1074636 B1 EP 1074636B1 EP 00116579 A EP00116579 A EP 00116579A EP 00116579 A EP00116579 A EP 00116579A EP 1074636 B1 EP1074636 B1 EP 1074636B1
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Prior art keywords
alloy
use according
aluminum alloy
iron
fraction
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EP00116579A
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German (de)
French (fr)
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EP1074636A1 (en
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Peter Dr. Czarnowski Von
Christian Dr. Dumont
Dirk Dr. Uffelmann
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Hydro Aluminium Deutschland GmbH
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Hydro Aluminium Deutschland GmbH
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Priority claimed from DE19948820A external-priority patent/DE19948820B4/en
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium

Definitions

  • the invention relates to the use of aluminum alloy sheet with a Alloy content of aluminum greater than 97% for the Shielding heat in motor vehicles.
  • Al 99.5 has, in addition to aluminum, the following alloying proportions within the specified limits: alloy component Value-up silicon 0.25% copper 0.05% magnesium 0.05% zinc 0.07% manganese 0.05% titanium 0.05% other 0.03%
  • Al 99.5 is advantageous from the viewpoints of high heat shielding and high formability, it is problematic at the same time from various other aspects.
  • Al 99.5 has a low strength.
  • the low strength of Al 99.5 results in that to ensure the required strength sheet metal parts must be used with greater thickness, which on the one hand increases the cost and on the other hand increases the weight of the ablebleches.
  • the low thermal stability of Al 99.5 creep sets in at temperatures above 150 ° C - leads to a low dimensional stability in use, but to maintain the distances of the heat shield against, for example, a catalyst and a vehicle underbody to ensure the desired heat shield necessary is.
  • Al 99.5 due to the high elongation values, as already mentioned a good thermoformability.
  • the yield strength is low at about 30 N / mm 2 .
  • the low yield strength of Al 99.5 limits the possibilities during the forming process in the production of heat shields.
  • the dynamic load pickups are made of Al 99.5 manufactured heat shields due to the strong Coarse grain formation inadequate.
  • the structural Reasons for desirable use of Noppenblechen is in connection with the use of Al 99.5 problematic because a dimensional stability is not guaranteed can be. This dimensional stability is characterized impaired that in Noppenblechen to the formed Pimple areas with increased coarse grain formation must be expected after a heat load.
  • the invention is based on the object, a To provide aluminum alloy for the shielding of heat in motor vehicles, the compared to Al 99.5 a further improved formability, an improved strength, a higher thermal Stability and less tendency to coarse grain formation having.
  • Overweight of iron and optionally manganese according to the invention thus of at most two for Al 99.5 according to DIN permissible main alloy components compared to those permitted by DIN for Al 99.5 Residual alloy components ensures that the Aluminum alloy used in the invention clearly more homogeneous structure, whereby the strength and the stretchability is improved and at the same time the The tendency to coarse grain formation is reduced. simultaneously the elasticity remains at least at the same level.
  • used aluminum alloy will double the Yield strength while increasing strength up to 50% by ensuring that the sum of the Alloy shares of skin plucking components Sum of the alloy shares of the remaining alloy components by at least a factor of 10.
  • An inventive aluminum alloy to be used with a particularly high yield strength and good strength against Al 99.5 constant elongation is ensured by the fact that Iron and manganese form the skin plucking components.
  • An optimization of yield strength and strength is in an aluminum alloy used according to the invention thereby ensures that the alloy content of manganese between 0.35% and 0.45%.
  • An aluminum alloy used in the invention in the iron the only main alloy component forms, has a compared to Al 99.5 improved yield strength and strength at the same time improved extensibility.
  • Aluminum alloy are used both in the event that iron and manganese form the main alloying components as well in the event that iron is the only one Main alloy component forms, thereby ensuring that the alloy content of iron is between 1.25% and 1.35%.
  • the alloying fraction of aluminum is at least 98%.
  • the alloying content of silicon is not 0.2% ensures that the desired Increasing the yield strength and strength at at least constant extensibility and reduced Coarse grain formation is achieved. For the same reasons it is advantageous if the alloy content of magnesium 0.003% and / or the alloy content of zinc 0.03 not exceeds.
  • alloy component Value of Value-up silicon 0.05% 0.1% copper 0.0% 0.05% magnesium 0.0% 0.003% zinc 0.0% 0.03% boron 0.0% 0.002% sodium 0.0% 0.001% lithium 0.0% 0.0002% iron 1.25% 1.35% manganese 0.35% 0.45% chrome 0.0% 0.02% titanium 0.0% 0.03% beryllium 0.0% 0.0% calcium 0.0% 0.001%
  • alloy contents for a first exemplary embodiment of an aluminum alloy used according to the invention which has a yield strength of about 110 N / mm 2 , a breaking strength of 124 N / mm 2 and an elongation of about 45%, will now be given below.
  • the alloying proportions for such an aluminum alloy are as follows: alloy content Alloy component silicon 0.063% copper 0.005% magnesium 0.0016% zinc 0.0036% boron 0.001% sodium ⁇ 0.001% iron 1.34% manganese 0.37% chrome 0.0014% titanium 0.019%
  • alloying components for a second exemplary embodiment of an aluminum alloy used according to the invention which has a yield strength of about 66 N / mm 2 , a strength of about 108 N / mm 2 and an extensibility of about 52%, are now given below.
  • the alloy components for such an aluminum alloy are as follows: alloy content alloy component silicon 0.08% copper 0.004% magnesium 0.0021% zinc 0.0044% boron 0.001% sodium ⁇ 0.001% iron 1.3% manganese 0.014% chrome 0.0012% titanium 0.02%

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Laminated Bodies (AREA)
  • Body Structure For Vehicles (AREA)
  • Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
  • Reinforced Plastic Materials (AREA)
  • Building Environments (AREA)
  • Cookers (AREA)

Abstract

The sum of alloying proportions of at most 2 main alloy components exceeds the sum of the alloying proportions of the remaining alloying components by at least a factor of 5.

Description

Die Erfindung betrifft die Verwendung von Blech aus einer Aluminiumlegierung mit einem Legierungsanteil von Aluminium größer als 97% für das Abschirmen von Wärme in Kraftfahrzeugen.The invention relates to the use of aluminum alloy sheet with a Alloy content of aluminum greater than 97% for the Shielding heat in motor vehicles.

Aufgrund der für eine Wärmeabschirmung besonders vorteilhaften physikalischen Eigenschaften von Aluminium - hoher Reflektionsgrad im Infrarot-Bereich und sehr gute Wärmeleitfähigkeit - haben sich Aluminiumlegierungen als Werkstoff zur Herstellung von Wärmeabschirmblechen als Standardlösung durchgesetzt. Um die genannten physikalischen Eigenschaften des Aluminium umfangreich zu nutzen und den hohen Anforderungen an die Umformbarkeit des Werkstoffes bei der Herstellung von Wärmeabschirmblechen gerecht zu werden, werden zur Zeit etwa 80% der Wärmeabschirmbleche in Al 99,5 (AA1050) gefertigt. Eine hinreichend gute Umformbarkeit dieses Werkstoffs durch Tiefziehen ist gewährleistet, da die Dehnung (A5) von Al 99,5 bei etwa 45% liegt.Due to the especially for a heat shield advantageous physical properties of aluminum - High reflectance in the infrared range and very good Thermal conductivity - have aluminum alloys as Material for the production of heat shields as Standard solution enforced. To the mentioned physical properties of the aluminum extensively too use and the high demands on the formability of the material in the production of To meet heat shields, are currently about 80% of the heat shields in Al 99.5 (AA1050) manufactured. A sufficiently good formability of this Material by deep drawing is guaranteed, as the Elongation (A5) of Al 99.5 is about 45%.

Nach DIN weist Al 99,5 neben Aluminium folgende Legierungsanteile in den angegebenen Grenzen auf: Legierungskomponente Wert-bis Silizium 0,25% Kupfer 0,05% Magnesium 0,05% Zink 0,07% Mangan 0,05% Titan 0,05% Sonstige 0,03% According to DIN, Al 99.5 has, in addition to aluminum, the following alloying proportions within the specified limits: alloy component Value-up silicon 0.25% copper 0.05% magnesium 0.05% zinc 0.07% manganese 0.05% titanium 0.05% other 0.03%

Die Verwendung von Al 99,5 ist zwar unter den Gesichtspunkten hohe Wärmeabschirmung und hohe Umformbarkeit vorteilhaft, gleichzeitig jedoch unter verschiedenen anderen Aspekten problematisch. Zum einen weist Al 99,5 eine geringe Festigkeit auf. Beim Einsatz von Wärmeabschirmblechen im Kraftfahrzeugbau werden jedoch erhebliche Anforderungen an die Festigkeit gestellt, die sich beispielsweise aus den Einwirkungen des Fahrtwindes oder von Spritzwasser bei hohen Geschwindigkeiten sowie der Einwirkung von Steinschlag ergeben. Die geringe Festigkeit von Al 99,5 führt dazu, daß zur Gewährleistung der erforderlichen Festigkeit Blechformteile mit größerer Dicke eingesetzt werden müssen, was einerseits die Kosten erhöht und andererseits das Gewicht des Wärmeabschirmbleches vergrößert. Die geringe thermische Stabilität von Al 99,5 - Kriechen setzt bereits bei Temperaturen von über 150 °C ein - führt zu einer im Einsatz geringen Formstabilität, die jedoch zur Einhaltung der Abstände des Wärmeabschirmbleches gegenüber beispielsweise einem Katalysator und einem Fahrzeugunterboden zur Gewährleistung der erwünschten Wärmeabschirmung notwendig ist. Al 99,5 weist aufgrund der hohen Dehnungswerte, wie bereits erwähnt eine gute Tiefziehbarkeit auf. Die Dehngrenze ist mit etwa 30 N/mm2 jedoch gering. Die geringe Dehngrenze von Al 99,5 begrenzt die Möglichkeiten während des Umformprozesses bei der Herstellung von Wärmeabschirmblechen.Although the use of Al 99.5 is advantageous from the viewpoints of high heat shielding and high formability, it is problematic at the same time from various other aspects. On the one hand Al 99.5 has a low strength. However, when heat shields are used in motor vehicle construction, considerable demands are placed on the strength, which results, for example, from the effects of the wind or splashing at high speeds and the effect of falling rocks. The low strength of Al 99.5 results in that to ensure the required strength sheet metal parts must be used with greater thickness, which on the one hand increases the cost and on the other hand increases the weight of the Wärmeabschirmbleches. The low thermal stability of Al 99.5 creep sets in at temperatures above 150 ° C - leads to a low dimensional stability in use, but to maintain the distances of the heat shield against, for example, a catalyst and a vehicle underbody to ensure the desired heat shield necessary is. Al 99.5, due to the high elongation values, as already mentioned a good thermoformability. However, the yield strength is low at about 30 N / mm 2 . The low yield strength of Al 99.5 limits the possibilities during the forming process in the production of heat shields.

Ein weiteres Problem insbesondere im Dauereinsatz von Wärmeabschirmblechen besteht darin, daß Al 99,5 eine hohe Neigung zur Grobkornbildung insbesondere nach geringen Kaltumformungen aufweist. Diese Grobkornbildung, insbesondere bei der zwangsläufigen thermischen Belastung von Wärmeabschirmblechen, führt dazu, daß speziell in Radien die Gefahr einer Rißentstehung beispielsweise in Befestigungspunkten des Wärmeabschirmbleches besteht. Another problem especially in continuous use of Wärmeabschirmblechen is that Al 99.5 a high Tendency to coarse grain formation, especially after low Has cold transformations. This coarse grain, especially with the inevitable thermal load of heat shields, causes that specifically in Radii the risk of cracking, for example, in Attachment points of the Wärmeabschirmbleches exists.

Auch sind die dynamischen Lastaufnahmen von aus Al 99,5 gefertigten Wärmeabschirmblechen aufgrund der starken Grobkornbildung unzureichend. Die aus strukturellen Gründen an sich erwünschte Verwendung von Noppenblechen ist in Verbindung mit dem Einsatz von Al 99,5 problematisch, da eine Formstabilität nicht gewährleistet werden kann. Diese Formstabilität wird dadurch beeinträchtigt, daß bei Noppenblechen an den umgeformten Noppenbereichen mit einer verstärkten Grobkornbildung nach einer Wärmebelastung gerechnet werden muß.Also, the dynamic load pickups are made of Al 99.5 manufactured heat shields due to the strong Coarse grain formation inadequate. The structural Reasons for desirable use of Noppenblechen is in connection with the use of Al 99.5 problematic because a dimensional stability is not guaranteed can be. This dimensional stability is characterized impaired that in Noppenblechen to the formed Pimple areas with increased coarse grain formation must be expected after a heat load.

Ausgehend von dem zuvor beschriebenen Stand der Technik liegt der Erfindung die Aufgabe zugrunde, eine Aluminiumlegierung für das Abschirmen von Wärme in Kraftfahrzeugen zur Verfügung zu stellen, die gegenüber Al 99,5 eine weiter verbesserte Umformbarkeit, eine verbesserte Festigkeit, eine höhere thermische Stabilität und eine geringere Neigung zur Grobkornbildung aufweist.Based on the previously described prior art The invention is based on the object, a To provide aluminum alloy for the shielding of heat in motor vehicles, the compared to Al 99.5 a further improved formability, an improved strength, a higher thermal Stability and less tendency to coarse grain formation having.

Erfindungsgemäß ist die zuvor hergeleitete und aufgezeigte Aufgabe dadurch gelöst, daß Blech aus einer Aluminiumlegierung mit einem Legierungsanteil von Aluminium größer als 97% für das Abschirmen von Wärme in Kraftfahrzeugen verwendet wird, wobei Eisen und gegebenenfalls Mangan die einzigen Hauptlegierungskomponenten bilden und deren Legierungsanteil die Summe der Legierungsanteile der Restlegierungskomponenten um mindestens den Faktor 5 übersteigt. Durch die erfindungsgemäße Übergewichtung von Eisen und gegebenenfalls Mangan, somit von höchstens zwei für Al 99,5 nach DIN zulässigen Hauptlegierungskomponenten gegenüber den nach DIN für Al 99,5 zulässigen Restlegierungskomponenten ist gewährleistet, daß die erfindungsgemäß verwendete Aluminiumlegierung ein deutlich homogeneres Gefüge aufweist, wodurch die Festigkeit und die Streckziehbarkeit verbessert ist und gleichzeitig die Neigung zur Grobkornbildung reduziert ist. Gleichzeitig bleibt die Dehnbarkeit zumindest auf gleichem Niveau. Gemäß einer ersten Ausgestaltung der erfindungsgemäßen verwendeten Aluminium-Legierung wird eine Verdoppelung der Streckgrenze bei gleichzeitiger Erhöhung der Festigkeit um bis zu 50% dadurch gewährleistet, daß die Summe der Legierungsanteile der Hautplegierungskomponenten die Summe der Legierungsanteile der Restlegierungskomponenten um mindestens den Faktor 10 übersteigt.According to the invention, the previously derived and indicated task solved in that Aluminum alloy sheet with an aluminum alloy content greater than 97% is used for shielding heat in motor vehicles, with iron and possibly manganese being the only ones Main alloy components and their alloying content is the sum of Alloy shares of the remaining alloy components um exceeds at least the factor 5. By the Overweight of iron and optionally manganese according to the invention, thus of at most two for Al 99.5 according to DIN permissible main alloy components compared to those permitted by DIN for Al 99.5 Residual alloy components ensures that the Aluminum alloy used in the invention clearly more homogeneous structure, whereby the strength and the stretchability is improved and at the same time the The tendency to coarse grain formation is reduced. simultaneously the elasticity remains at least at the same level. According to a first embodiment of the invention used aluminum alloy will double the Yield strength while increasing strength up to 50% by ensuring that the sum of the Alloy shares of skin plucking components Sum of the alloy shares of the remaining alloy components by at least a factor of 10.

Eine erfindungsgemäß zu verwendende Aluminiumlegierung mit besonders hoher Streckgrenze und guter Festigkeit bei gegenüber Al 99,5 gleichbleibender Dehnung ist dadurch gewährleistet, daß Eisen und Mangan die Hautplegierungskomponenten bilden.An inventive aluminum alloy to be used with a particularly high yield strength and good strength against Al 99.5 constant elongation is ensured by the fact that Iron and manganese form the skin plucking components.

Eine Optimierung der Streckgrenze und der Festigkeit ist bei einer erfindungsgemäß verwendeten Aluminiumlegierung dadurch gewährleistet, daß der Legierungsanteil von Mangan zwischen 0,35% und 0,45% liegt.An optimization of yield strength and strength is in an aluminum alloy used according to the invention thereby ensures that the alloy content of manganese between 0.35% and 0.45%.

Eine erfindungsgemäß verwendete Aluminiumlegierung bei der Eisen die einzige Hauptlegierungskomponente bildet, weist eine gegenüber Al 99,5 verbesserte Streckgrenze und Festigkeit bei gleichzeitig verbesserter Dehnbarkeit auf.An aluminum alloy used in the invention in the iron the only main alloy component forms, has a compared to Al 99.5 improved yield strength and strength at the same time improved extensibility.

Die Eigenschaften einer erfindungsgemäß verwendeten Aluminiumlegierung werden sowohl für den Fall, daß Eisen und Mangan die Hauptlegierungskomponenten bilden als auch für den Fall, daß Eisen die einzige Hauptlegierungskomponente bildet, dadurch gewährleistet, daß der Legierungsanteil von Eisen zwischen 1,25% und 1,35% liegt.The properties of a used according to the invention Aluminum alloy are used both in the event that iron and manganese form the main alloying components as well in the event that iron is the only one Main alloy component forms, thereby ensuring that the alloy content of iron is between 1.25% and 1.35%.

Um die für Wärmeabschirmbleche vorteilhaften physikalischen Eigenschaften des Aluminiums möglichst umfangreich zu nutzen, ist es vorteilhaft, daß bei einer erfindungsgemäß verwendeten Aluminiumlegierung der Legierungsanteil von Aluminium mindestens 98% beträgt.To those advantageous for heat shields physical properties of the aluminum as possible extensive use, it is advantageous that at one Aluminum alloy used according to the invention, the alloying fraction of aluminum is at least 98%.

Dadurch, daß der Legierungsanteil von Silizium 0,2% nicht übersteigt, ist gewährleistet, daß die erwünschte Erhöhung der Streckgrenze und der Festigkeit bei zumindest gleichbleibender Dehnbarkeit und reduzierter Grobkornbildung erreicht wird. Aus denselben Gründen ist es vorteilhaft, wenn der Legierungsanteil von Magnesium 0,003% und/oder der Legierungsanteil von Zink 0,03 nicht übersteigt.Because the alloying content of silicon is not 0.2% ensures that the desired Increasing the yield strength and strength at at least constant extensibility and reduced Coarse grain formation is achieved. For the same reasons it is advantageous if the alloy content of magnesium 0.003% and / or the alloy content of zinc 0.03 not exceeds.

Die nach DIN für Al 99,5 ebenfalls zulässigen Legierungsanteile Chrom und Titan beeinträchtigen die erwünschten Eigenschaften der erfindungsgemäß verwendeten Aluminiumlegierung auch oberhalb der nach DIN vorgegebenen Legierungsanteile zunächst nicht. Zur Gewährleistung der erwünschten Eigenschaften der erfindungsgemäß verwendeten Aluminiumlegierung ist es jedoch vorteilhaft, wenn der Legierungsanteil von Titan 0,03% und/oder der Legierungsanteil von Chrom 0,02% nicht übersteigt.The also permitted according to DIN for Al 99.5 Alloy shares chrome and titanium affect the desired properties of the invention used Aluminum alloy also above the DIN initially not given alloy shares. to Ensuring the desired properties of However, it is the aluminum alloy used in the present invention advantageous if the alloy content of titanium is 0.03% and / or the alloying level of chromium 0.02% not exceeds.

Die Legierungsanteile der weiteren nach DIN zulässigen Legierungskomponenten Kupfer, Natrium und Kalzium beeinträchtigen in den nach DIN zulässigen Legierungsanteilen die erfindungsgemäß gewährleisteten Eigenschaften nur geringfügig.The alloying shares of the others permitted by DIN Alloy components copper, sodium and calcium impair in the permissible according to DIN Alloy shares guaranteed according to the invention Properties only slightly.

Es gibt nun eine Vielzahl von Möglichkeiten, die erfindungsgemäß verwendete Aluminiumlegierung zur Herstellung von Wärmeabschirmblechen auszugestalten und weiterzubilden. Hierzu wird beispielsweise einerseits verwiesen auf die dem Patentanspruch 1 nachgeordneten Patentansprüche andererseits auf die folgende Beschreibung von vorteilhaften Legierungszusammensetzungen:There are now a lot of ways that Aluminum alloy used according to the invention for the production of Design and develop heat shields. For this purpose, for example, referenced on the one hand The patent claim 1 subordinate claims on the other hand, to the following description of advantageous alloy compositions:

Eine etwa auf 100 N/mm2 verbesserte Dehngrenze ist mit einer Aluminiumlegierung mit Anteilen von den auch nach DIN für Al 99,5 zugelassenen Legierungskomponenten innerhalb der folgenden Grenzen gewährleistet: Legierungskomponente Wert-von Wert-bis Silizium 0,05% 0,1% Kupfer 0,0% 0,05% Magnesium 0,0% 0,003% Zink 0,0% 0,03% Bor 0,0% 0,002% Natrium 0,0% 0,001% Lithium 0,0% 0,0002% Eisen 1,25% 1,35% Mangan 0,35% 0,45% Chrom 0,0% 0,02% Titan 0,0% 0,03% Beryllium 0,0% 0,0% Kalzium 0,0% 0,001% An improved yield strength of approximately 100 N / mm 2 is ensured with an aluminum alloy with proportions of the alloy components also approved according to DIN for Al 99.5 within the following limits: alloy component Value of Value-up silicon 0.05% 0.1% copper 0.0% 0.05% magnesium 0.0% 0.003% zinc 0.0% 0.03% boron 0.0% 0.002% sodium 0.0% 0.001% lithium 0.0% 0.0002% iron 1.25% 1.35% manganese 0.35% 0.45% chrome 0.0% 0.02% titanium 0.0% 0.03% beryllium 0.0% 0.0% calcium 0.0% 0.001%

Innerhalb der vorgegebenen Grenzen können die Legierungsanteile zur Einstellung verschiedener Eigenschaften der Aluminiumlegierung gezielt variiert werden.Within the given limits, the Alloy shares for setting various Properties of the aluminum alloy varied specifically become.

Im folgenden werden nun die Legierungsanteile für ein erstes Ausführungsbeispiel einer erfindungsgemäß verwendeten Aluminiumlegierung angegeben, die eine Dehngrenze von etwa 110 N/mm2, eine Bruchfestigkeit von 124 N/mm2 und eine Dehnung von etwa 45% aufweist. Die Legierungsanteile für eine derartige Aluminiumlegierung lauten wie folgt: Legierungsanteil Legierungs komponente Silizium 0,063% Kupfer 0,005% Magnesium 0,0016% Zink 0,0036% Bor 0,001% Natrium <0,001% Eisen 1,34% Mangan 0,37% Chrom 0,0014% Titan 0,019% The alloy contents for a first exemplary embodiment of an aluminum alloy used according to the invention, which has a yield strength of about 110 N / mm 2 , a breaking strength of 124 N / mm 2 and an elongation of about 45%, will now be given below. The alloying proportions for such an aluminum alloy are as follows: alloy content Alloy component silicon 0.063% copper 0.005% magnesium 0.0016% zinc 0.0036% boron 0.001% sodium <0.001% iron 1.34% manganese 0.37% chrome 0.0014% titanium 0.019%

Im folgenden werden nun die Legierungsanteile für ein zweites Ausführungsbeispiel einer erfindungsgemäß verwendeten Aluminiumlegierung angegeben, die eine Streckgrenze von etwa 66 N/mm2, eine Festigkeit von etwa 108 N/mm2 und eine Dehnbarkeit von etwa 52% aufweist. Die Legierunsganteile für eine derartige Aluminiumlegierung lauten wie folgt: Legierungsanteil Legierungskomponente Silizium 0,08% Kupfer 0,004% Magnesium 0,0021% Zink 0,0044% Bor 0,001% Natrium <0,001% Eisen 1,3% Mangan 0,014% Chrom 0,0012% Titan 0,02% The alloying components for a second exemplary embodiment of an aluminum alloy used according to the invention, which has a yield strength of about 66 N / mm 2 , a strength of about 108 N / mm 2 and an extensibility of about 52%, are now given below. The alloy components for such an aluminum alloy are as follows: alloy content alloy component silicon 0.08% copper 0.004% magnesium 0.0021% zinc 0.0044% boron 0.001% sodium <0.001% iron 1.3% manganese 0.014% chrome 0.0012% titanium 0.02%

Claims (12)

  1. Use of sheet metal made of aluminium alloy having an aluminium alloy fraction higher than 97 % for the shielding of heat in motor vehicles, wherein iron and possibly manganese form the only main alloying components and their alloy fraction exceeds the sum of the alloy fractions of the remaining alloying components by at least the factor 5.
  2. The use of sheet metal made of aluminium alloy according to claim 1, characterised in that the sum of the alloy fractions of the main alloying components exceeds the sum of the alloy fractions of the remaining alloying components by at least the factor 10.
  3. The use according to claim 1 or 2, characterised in that iron and manganese form the main alloying components.
  4. The use according to claim 3, characterised in that the alloy fraction of manganese is between 0.35 % and 0.45 %.
  5. The use according to claim 1 or 2, characterised in that iron forms the only main alloying component.
  6. The use according to any one of claims 3 to 5, characterised in that the alloy fraction of iron is between 1.25 % and 1.35 %.
  7. The use according to any one of claims 1 to 6, characterised in that the alloy fraction of aluminium is at least 98 %.
  8. The use according to any one of claims 1 to 7, characterised in that the alloy fraction of silicon does not exceed 0.2 %.
  9. The use according to any one of claims 1 to 8, characterised in that the alloy fraction of magnesium does not exceed 0.003 %.
  10. The use according to any one of claims 1 to 9, characterised in that the alloy fraction of zinc does not exceed 0.03 %.
  11. The use according to any one of claims 1 to 10, characterised in that the alloy fraction of titanium does not exceed 0.03 %.
  12. The use according to any one of claims 1 to 12, characterised in that the alloy fraction of chromium does not exceed 0.02 %.
EP00116579A 1999-08-05 2000-08-01 Use of aluminum alloy sheet for heat shielding Expired - Lifetime EP1074636B1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE19936234 1999-08-05
DE19936234 1999-08-05
DE19948820 1999-10-09
DE19948820A DE19948820B4 (en) 1999-08-05 1999-10-09 Heat shield made of an aluminum alloy

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EP1074636A1 EP1074636A1 (en) 2001-02-07
EP1074636B1 true EP1074636B1 (en) 2005-03-23

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EP (1) EP1074636B1 (en)
AT (1) ATE291646T1 (en)
CZ (1) CZ296688B6 (en)
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JP5004007B2 (en) * 2007-04-12 2012-08-22 日本軽金属株式会社 Aluminum alloy plate for battery lid and manufacturing method thereof
CN111893349A (en) * 2014-07-09 2020-11-06 海德鲁铝业钢材有限公司 Application of aluminum alloy or flat aluminum product composed of aluminum alloy to aluminum-plastic composite component

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CH654027A5 (en) * 1983-08-23 1986-01-31 Alusuisse METHOD FOR PRODUCING FINE-GRINED ALUMINUM ROLLING PRODUCTS.
DD224874A1 (en) * 1984-06-21 1985-07-17 Mansfeld Kom W Pieck Fi F Ne M ALUMINUM ALLOYING AND METHOD FOR PROCESSING THE ALLOY
CH684206A5 (en) * 1990-11-12 1994-07-29 Matec Holding Disposable heat shield.
US5380379A (en) * 1993-08-18 1995-01-10 Alcoa Aluminio Do Nordeste S.A. Aluminum foil product and manufacturing method

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ATE291646T1 (en) 2005-04-15
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EP1074636A1 (en) 2001-02-07
CZ296688B6 (en) 2006-05-17
PT1074636E (en) 2005-07-29

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